session IP

Title: Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM
type: interactive
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Astrodynamics addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.

IPC members

Co-Chair: Dr. Diane Davis, National Aeronautics and Space Administration (NASA), Johnson Space Center, United States;
Co-Chair: Dr. Florian Renk, European Space Agency (ESA), Germany;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Dynamic analysis of mechanical motion of a variable-mass rocket system	10	confirmed	Prof.Dr. Valeh Bakhshali	Azerbaijan Technical University	Azerbaijan
Dynamic modelling and drag-free control system design for the space-borne gravitational wave detector in the port-Hamiltonian framework	10	withdrawn	Mr. Haojun Ma	National Space Science Center, Chinese Academy of Sciences;University of Chinese Academy of Sciences	China
Desensitized Ensemble Guidance	10	confirmed	Prof. Ismail Bayezit	Istanbul Technical University	Türkiye
Machine Learning Based Guidance for Optimal Spacecraft De-Orbiting	10	confirmed	Ms. Emanuela Gaglio	Scuola Superiore Meridionale	Italy
optimization of low-energy trajectories to the Earth-Moon L2 halo orbit with finite thrust via parameter continuation method	10	withdrawn	Mr. Rui Zhou	Moscow Aviation Institute (National Research University, MAI)	Russian Federation
Comparison of Non-Linear Heuristic Control and Linear Time-Varying Optimal Control Design for 3-axes Attitude Control of a Microsatellite	10	confirmed	Ms. Neha Chohan	ReOrbit	Finland
Closed-loop guidance for interplanetary CubeSats with indirect methods	10	confirmed	Mrs. Alessandra Mannocchi	Politecnico di Milano	Italy
Robust low-thrust gravity-assist trajectory optimization	10	confirmed	Mr. Jin Cheng Hu	Nanjing University of Aeronautics and Astronautics	China
Optimal Tuning of the Nanosatellite Attitude Controller Using TRIAD-Aided Kalman Filter and Particle Swarm Optimization	10	confirmed	Prof.Dr. Chingiz Hajiyev	Istanbul Technical University	Türkiye
THE EXTENDED WAHBA’S PROBLEM IN DUAL AND MULTIDUAL QUATERNIONS	10	confirmed	Prof. Daniel Condurache	Technical University of Iasi	Romania
Approximation for gravitational field of a small celestial body by a triple of uniform balls	10	confirmed	Prof. Anna Guerman	Centre for Mechanical and Aerospace Science and Technologies (C-MAST)	Portugal
Multiple Fly-By Low Thrust Trajectory Design Using Finite Fourier Series Shape-Based Approach	10	withdrawn	Ms. Dhanisha Sateesh	Space Generation Advisory Council (SGAC)	India
Trajectory Planning and Execution in a Hyper Redundant Continuum Manipulator for Satellite Docking	10	confirmed	Mr. Ayush Ranjan	Indian Institute of Technology Kanpur	India
Optimal control of the thrust vector of a spacecraft with an air-breathing electric propulsion	10	confirmed	Prof. Alexander S. Filatyev	Lomonosov Moscow State University	Russian Federation
Fuel-Minimum Fuel-Average Control Algorithm for Large Constellation Configuration Maintenance Based on Perturbation Compensation Method	10		Dr. Simeng Huang		China
Minimum-Propellant Direct, Assisted, and Slingshot Return Trajectories from Mars, Jupiter, and their moons	10	confirmed	Mr. Alessio Patti	Politecnico di Torino	Italy
Attitude determination and control system design for a 3U CubeSat to monitor forward light scattering over Earth horizon	10	confirmed	Mr. Mehmet Esit	Kyushu Institute of Technology	Japan
Overcoming Challenges: Achieving Formation Flying for SIGNIT with Limited Space Situational Awareness and Propulsion Systems	10	withdrawn	Mr. Eric Bertels	ISIS - Innovative Solutions In Space B.V.	The Netherlands
Guidance, Navigation and Control for the autonomous rendezvous and docking of cooperative targets	10	withdrawn	Mr. Alvaro Martinez	SENER Aeroespacial	Spain
Three-body Moon-Mars transfer with revisited weak stability boundary concept and aerobraking capture	10	confirmed	Mr. Gabriele Mocciola	Politecnico di Torino	Italy
Intelligent Integrated Navigation of Solar System Boundary Exploration Cruise Phase Based on Q-Learning Extended Kalman Filter	10	confirmed	Mr. Hui Wang	School of aeronautics and astronautics, Sun Yat-Sen University Guangzhou	China
Robust Attitude Control Using Electrospray Thruster	10		Mr. Gianni Pecora	Politecnico di Torino	Italy
Variable-Performance Electrospray Maneuvers Optimization	10		Mr. Giuseppe Di Pasquale	IENAI SPACE	Spain
using the dzhanibekov effect to generate angular acceleration for hardware correcting maneuvers	10	withdrawn	Mr. Johannes Ihle	NTNU	Norway
Attitude and orbit control of a geostationary satellite during North-South Station keeping	10	withdrawn	Dr. ELHASSEN BENFRIHA	Agence Spatiale Algérienne (ASAL)	Algeria
Time-delay flight control of small-scale vertical take-off and vertical landing demonstrator using a mini gas turbine engine	10	confirmed	Mr. Minwoo Kim	Korea Aerospace University	Korea, Republic of
Design of transfer trajectories from cislunar orbits to the retrograde Geo-Synchronous Orbit	10	confirmed	Mr. Yuchen He	Beihang University	China

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